[go: up one dir, main page]

EP1005945A2 - Laser-beam machining method, laser-beam machining device and auxiliary tool for piercing - Google Patents

Laser-beam machining method, laser-beam machining device and auxiliary tool for piercing Download PDF

Info

Publication number
EP1005945A2
EP1005945A2 EP99307625A EP99307625A EP1005945A2 EP 1005945 A2 EP1005945 A2 EP 1005945A2 EP 99307625 A EP99307625 A EP 99307625A EP 99307625 A EP99307625 A EP 99307625A EP 1005945 A2 EP1005945 A2 EP 1005945A2
Authority
EP
European Patent Office
Prior art keywords
nozzle
piercing
hole
machining
laser
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP99307625A
Other languages
German (de)
French (fr)
Other versions
EP1005945A3 (en
Inventor
Yoshinori Nakata
Tadashi Fanuc Dai3virakaramatsu Kurosawa
Atsushi Room 8-103 Fanuc Manshonharimomi Mori
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fanuc Corp
Original Assignee
Fanuc Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fanuc Corp filed Critical Fanuc Corp
Publication of EP1005945A2 publication Critical patent/EP1005945A2/en
Publication of EP1005945A3 publication Critical patent/EP1005945A3/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/1462Nozzles; Features related to nozzles
    • B23K26/1482Detachable nozzles, e.g. exchangeable or provided with breakaway lines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/0665Shaping the laser beam, e.g. by masks or multi-focusing by beam condensation on the workpiece, e.g. for focusing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/142Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor for the removal of by-products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/1435Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor involving specially adapted flow control means
    • B23K26/1436Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor involving specially adapted flow control means for pressure control
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/1462Nozzles; Features related to nozzles
    • B23K26/1464Supply to, or discharge from, nozzles of media, e.g. gas, powder, wire
    • B23K26/1476Features inside the nozzle for feeding the fluid stream through the nozzle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/38Removing material by boring or cutting
    • B23K26/382Removing material by boring or cutting by boring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/40Removing material taking account of the properties of the material involved
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/02Iron or ferrous alloys
    • B23K2103/04Steel or steel alloys
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/50Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26

Definitions

  • This invention relates to a laser-beam machining method, a laser-beam machining device, and an auxiliary tool, for carrying out machining to pierce a cutting target such as a steel sheet.
  • a laser-beam machining method of cutting a machining target such as a steel sheet by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a nozzle having a small hole piercing work or boring work is required at the start of machining.
  • a serious problem faced during piercing is the presence of scattered dross. Since boring of a machining target such as steel sheet or the like is carried out by melting the machining target by laser beam while jetting assist gas through the nozzle, scattering of dross resulting from melting the machining target by the laser beam occurs due to the assist gas jetted through the nozzle. There is a danger that the scattered dross may be adhered to the nozzle to damage the nozzle or be adhered to an operator to burn the operator. Further, the scattered dross adhered to the surface of the machining target hinders the subsequent machining for the machining target.
  • the scattered dross is adhered to the surface of the machining target, resulting in the hindrance of the subsequent cutting.
  • a method of shielding a machining point to collect the dross in Japanese Patent Application Laid-open No. 9-271980.
  • this method is supposed to be used in association with piercing based on pulse output which is determined in advance in terms of such size and quantity of scattered dross as will enable the scattered dross to be absorbed and collected (See Japanese Patent Application Laid-open No. 5-185261).
  • An object of the present invention is to provide a laser-beam machining method, a laser-beam machining device and an auxiliary tool for piercing which permit piercing at high speed.
  • Another object of the present invention is to provide a laser-beam machining method, a laser-beam machining device and an auxiliary tool for piercing which may reduce scattered dross, resulting in less occurrence of adhesion of the dross to a machining target.
  • a nozzle having a hole diameter larger than a converged laser beam diameter and smaller than a hole diameter of a cuffing nozzle is used as a piercing nozzle.
  • the nozzle has a hole diameter preferably, but not essentially, of not more than 2.5 mm.
  • Piercing may be carried out on condition that an underlay formed by a metal sheet having a hole therein, possibly in the center, is placed on the machining target, so that the underlay is permitted to catch the scattered dross so as to avoid the dross from adhering to the surface of the machining target.
  • a piercing nozzle may be connected to the tip of a cutting nozzle at the time of piercing, for the reason that piercing carried out using a cutting or piercing nozzle having a relatively small hole diameter may shorten the time taken for the piercing and may cause less scattering of the dross, in comparison with the piercing carried out using a cutting nozzle having a relatively large hole diameter.
  • the piercing nozzle may be mounted to the cutting nozzle detachably, or may be mounted to be movable between a piercing position and a shunting position.
  • a clearance for cooling down the scattered dross may be provided between the piercing nozzle and an underlay. There may also be provided a blade driven in the clearance to remove the scattered dross from the surface of the underlay, and/or a scattered dross removing means to remove the scattered dross by flowing gas or a fluid into the clearance.
  • the piercing nozzle added to the cuffing nozzle, and the underlay may be provided in a pair as an auxiliary tool for piercing.
  • the laser-beam machining device comprises a cutting nozzle 1 normally used for cutting a machining target and a piercing nozzle 2 used in combination with the cutting nozzle 1 for piercing. Further, a pivotal portion 4 is provided on one end of the piercing nozzle 2, and an underlay 3 is mounted to the piercing nozzle 2 through the pivotal portion 4 so that it can rotate relative to and can be detached from the piercing nozzle 2.
  • a spacer 2b is provided in a projected state at four corners of the lower surface (i.e., the surface opposite to the surface brought into engagement with the cutting nozzle 1) of the piercing nozzle 2, so that when the underlay 3 is placed on the side of the piercing nozzle 2, a clearance 5 is formed between the piercing nozzle 2 and the underlay 3, as shown in Fig. 1.
  • the underlay 3 is used to prevent scattered dross from adhering to the surface of a machining target 6 at the time of piercing.
  • the underlay 3 has a hole 3a in the center.
  • the underlay 3 is placed in a manner such that the hole 3a and a hole 2a of the piercing nozzle 2 overlap with each other, in particular, in a manner such that the center of the hole 3a of the underlay 3 is placed in alignment with the center of the hole 2a of the piercing nozzle 2.
  • the upper surface of the piercing nozzle 2 has a tapered fitting hole 2c, to which the tip of the cutting nozzle 1 is capable of being fitted.
  • the tip of the cutting nozzle 1 has a nozzle hole 1a in the center. Further, the piercing hole 2a is formed to extend from the center of the tapered fitting hole 2c to the lower surface of the piercing nozzle 2.
  • a laser beam 10 passes through the nozzle hole 1a at the tip of the cutting nozzle 1, the piercing hole 2a and the hole 3a of the underlay 3 and then reaches the machining target 6.
  • the underlay 3 needs to have a size enough to cover the scattering range of the dross caused by the piercing.
  • a flat sheet in the shape of a square of 60 mm x 60 mm with a thickness of 3 mm is in use, and its material is the same copper alloy as the piercing nozzle 2.
  • the hole 3a formed in the underlay 3 is too large, the scattered dross will adhere to the surface of the machining target 6 at a portion corresponding to the hole 3a, and therefore, it is better to form the hole 3a as small as possible.
  • the hole 3a is too small, it will take a longer time disadvantageously to carry out piercing on account of reduction in an area of the part of machining target 6 where the assist gas 11 strikes, and so on.
  • the hole 3a of the underlay 3 which is larger than the hole 2a of the piercing nozzle 2 is found by an experiment or the like.
  • the hole 3a of the underlay 3 is formed to have a diameter of about 5 mm.
  • the clearance 5 between the underlay 3 and the piercing nozzle 2 is set to 3 mm.
  • the piercing nozzle 2 Since the piercing nozzle 2 is used for catching scattered dross above the underlay 3, its size is set to be substantially equal to that of the underlay 3.
  • the nozzle hole 2a of the piercing nozzle 2 is formed to be smaller in diameter than the nozzle hole 1a of the cutting nozzle 1. If the nozzle hole 2a has a larger diameter, an area of the part of machining target 6 where the assist gas 11 jetted through the nozzle hole 2a strikes is increased and injection speed of the assist gas is reduced, in comparison with the case where the nozzle hole 2a has a smaller diameter with the assist gas 20 supplied under the same pressure.
  • the nozzle hole 2a has a smaller diameter, the injection speed is increased and an area of the part of machining target 6 where the assist gas 11 strikes is reduced, in comparison with the case where the nozzle hole 2a has a larger diameter with the assist gas 11 supplied under the same pressure.
  • diameter of the nozzle hole 2a is decreased, the force for scattering the dross of the machining target melted in the process of piercing is increased, bringing about quick scattering of the dross caused by the irradiation of the laser beam 10, with the result that the diameter of a hole machined by the piercing decreases and scattered dross decreases in quantity.
  • the nozzle hole 2a of the piercing nozzle 2 preferably needs to have a diameter larger than the diameter of converged laser beam 10 and smaller than the nozzle hole 1a of the cutting nozzle 1.
  • the nozzle hole 1a of the cutting nozzle 1 has a diameter of 4 mm, and the laser beam 10 has a converged spot diameter of about 0.8 mm
  • the nozzle hole 2a of the piercing nozzle 2 is formed to have a diameter of 1.5 mm (larger than 0.8 mm and smaller than 4 mm).
  • the length of the hole 2a of the piercing nozzle 2, which has diameter of 1.5 mm, is set to 10 mm. In piercing using this piercing nozzle 2, it is ascertained that it does not matter if the laser beam is reflected from the inner wall of the piercing nozzle 2.
  • the cutting nozzle 1 is put above a target position for machining to pierce the machining target 6. Subsequently, the tapered fitting hole 2c of the piercing nozzle 2 is fitted to the tip of the cutting nozzle 1 to combine the cutting nozzle 1 with the piercing nozzle 2 and the underlay 3. Then, the cutting nozzle 1, the piercing nozzle 2 and the underlay 3 are moved down in a combined state toward a piercing position on the machining target 6 such that the underlay 3 is placed on the surface of the machining target 6 as shown in Fig. 1.
  • the laser oscillator (not shown) is activated to irradiate the converged laser beam 10 to the machining target 6 through the hole 1a of the cutting nozzle 1, the hole 2a of the piercing nozzle 2 and the hole 3a of the underlay 3 (see Fig. 2A), while the injection of the assist gas 11 to the machining target 6 is carried out through the holes 1a, 2a and 3a.
  • the portion of the machining target 6, irradiated by the laser beam 10 starts melting.
  • the resultant dross is removed from the machining target 6 by high-speed and high-pressure assist gas 11 jetted through the small-diameter nozzle hole 2a of the piercing nozzle 2.
  • the assist gas 11 is turned in a reverse direction after striking against the machining target 6 and is then exhausted from the hole 3a of the underlay 3 to the outside through the clearance 5 between the piercing nozzle 2 and the underlay 3, while the dross carried by the assist gas 11 is cooled down in the course of the passage through the clearance 5 and is then dropped down to the underlay 3, resulting in the adhesion of the dross to the underlay 3.
  • the assist gas 11 is jetted at high speed under high pressure to a narrow area of the machining target 6 through the small nozzle hole 2a of the piercing nozzle 2, the dross is removed from the machining target 6 at high speed, so that the laser beam 10 is allowed to melt the inner part of the machining target 6.
  • a hole machined by the piercing decreases in diameter, and the scattered dross also decreases in quantity.
  • the piercing nozzle 2 and the underlay 3 are removed from the cutting nozzle 1 to start the normal cutting with the cutting nozzle 1 (refer to Fig. 2B).
  • the piercing nozzle 2 and the underlay 3, having been removed from the cutting nozzle 1, is put in a ready state for the next piercing after opening the piercing nozzle 2 through the pivotal motion relative to the underlay 3 about the pivotal portion 4 or separating the underlay 3 from the piercing nozzle 2 and then scraping off the adhered dross from the underlay 3.
  • a cover 2b' is formed at the edge of the piercing nozzle 2, so that when the piercing nozzle 2 is placed opposite to the underlay 3, the cover 2b' serves as a spacer to form a clearance 5 of a predetermined depth between the piercing nozzle 2 and the underlay 3, and also to define the sectional shape of the clearance 5.
  • Fig. 3B is a view showing the piercing nozzle 2 of Fig. 3A as viewed from the bottom, after the removal of the underlay 3 placed below the piercing nozzle 2.
  • the clearance 5 has a substantially circular sectional shape.
  • the cover 2b' has three paths (a path leading to an exhaust port 21, a path leading to an inlet port 22 and a path leading to an injection port 23) which are formed in a parallel arrangement to permit the communication between the clearance 5 and the outside of the piercing nozzle 2.
  • the assist gas 11 in the clearance 5 is exhausted to the outside through the exhaust port 21.
  • a fluid such as compressed air is supplied from the outside into the clearance 5 through the inlet port 22.
  • Oil, a soap solution or a surface active solution is jetted or sprayed from the outside into the clearance 5 through the injection port 23.
  • the compressed air supplied into the clearance 5 through the inlet port 22 flows along the inner surface of the clearance 5 of the circular sectional shape to form a swirl flow and is then exhausted through the exhaust port 21.
  • the dross scattered by the assist gas 11 is cooled down by the compressed air and is then exhausted through the exhaust port 21. Since the dross is cooled down by the compressed air before being exhausted through the exhaust port 21 as described above, the quantity of dross adhered to the surface of the underlay 3, which is exhausted through the exhaust port 21 and then dropped down to the underlay 3, is decreased.
  • a fluid (gas or liquid) other than the compressed air may be supplied through the inlet port 22.
  • the scattered dross is covered and then cooled down with oil, soap solution or surface active solution which has been jetted into the clearance 5 through the injection port 23, the dross dropped down to the underlay 3 after having been cooled down is hardly adhered to the underlay 3, and as a result, is exhausted through the exhaust port 21 together with the compressed air supplied through the inlet port 22.
  • the piercing nozzle 2 and the underlay 3 may be used for a long time without being cared for. Further, even if the dross is adhered to the underlay 3, it is possible to easily remove the adhered dross from the underlay 3 by enclosing the adhered dross with the oil, the soap solution or the surface active solution.
  • the laser-beam machining device may carry out the piercing continuously without frequent operation for removing the dross.
  • the laser-beam machining device according to the third embodiment is equivalent to a laser-beam machining device having a plurality of blades 24 (six blades in the embodiment shown in Fig. 4B) provided in a rotatable state in the clearance 5 of the laser-beam machining device according to the second embodiment.
  • These blades 24 are mounted on the piercing nozzle 2 at the center portion thereof (a portion surrounding the nozzle hole 2a) through a ball bearing 25 so that they can rotate. More specifically, as shown in Fig. 4A, a cylindrical projection projecting toward the clearance 5 is formed in the center of the piercing nozzle 2, and an inner race of the ball bearing 25 is fixed to the projection. On the other hand, these six blades 24 are fixed to the outer race of the ball bearing 25.
  • These blades 24 are rotated by the compressed air supplied into the clearance 5 through the inlet port 22 in the course of piercing.
  • dross caused by irradiation of the laser beam 10 and then scattered by the assist gas 11 is carried toward the exhaust port 21 together with the assist gas through the rotation of the blades 24 while being cooled down by the compressed air and is then exhausted through the exhaust port 21.
  • the rotating blades 24 carry the dross toward the exhaust port 21 after having scraped off from the underlay 3, and the dross is exhausted through the exhaust port 21.
  • the dross when carrying out piercing using the laser-beam machining device according to the third embodiment, since the dross is forcibly exhausted by the blades 24, the dross can not accumulate in the clearance 5, so that it is possible to carry out piercing continuously. Further, since the dross is not allowed to adhere and accumulate on the underlay 3, there is no need to frequently clean the underlay 3.
  • the underlay 3 and the piercing nozzle 2 are connected together pivotally through the pivotal means (the pivotal portion 4).
  • a fixing means such as a set screw is used to connect the underlay 3 and the piercing nozzle 2 together.
  • the compressed air is supplied into the clearance 5 through the inlet port 22.
  • fluid such as compressed air need not be supplied through the inlet port 22, or the inlet port 22 for supplying the fluid need not be formed in the cover 2b' of the piercing nozzle 2.
  • the assist gas 11 jetted at high speed under high pressure toward the machining target 6 is turned in the reverse direction after striking against the machining target 6 and then flows into the clearance 5 between the piercing nozzle 2 and the underlay 3, while the assist gas 11 in the clearance 5 forms a swirl flow and is then exhausted to the outside through the exhaust port 21 serving as the only outlet.
  • the swirl flow of the assist gas 11 causes the rotation of the blades 24.
  • connection of the piercing nozzle 2 to the cutting nozzle 1 is carried out only by fitting the tip of the cutting nozzle 1 to the tapered fitting hole 2a of the piercing nozzle 2 without any special attaching mechanism used.
  • FIG. 5 is a view of the cutting nozzle 1 mounted with the piercing nozzle 2 though the attaching mechanism, as viewed from the top. It should be noted that the piercing nozzle 2 mounted with the attaching mechanism as will be described later and the underlay 3 connected to this piercing nozzle 2 have the same structure as those of the laser-beam machining device according to the first, second and third embodiments.
  • the outer surface of the cutting nozzle 1 has a groove to which a pair of clips 33 (which will be described later) constituting a mounting mechanism are fitted.
  • a pair of shafts 31 are provided in a projected state on one side of the upper surface (i.e., the surface on the side opposite to the cutting nozzle 1) of the piercing nozzle 2, and the bases of the clips 33 are respectively mounted to the shafts 31 in a pivotal state. Further, a spring 32 is provided between these two clips 33, and these two clips 33 are energized to come close to each other by means of the spring 32.
  • Each clip 33 has a tapered end, and a distance between the inner edge of one clip 33 and the inner edge of the other clip 33 gradually widens toward the ends of the clips. Then, when a removing member 34 is pressed against the ends of the clips 33 and is then pushed toward the cutting nozzle 1, the pair of clips 33 are expanded against the force of the spring 32 as shown by a broken line of Fig. 5.
  • the tip of the cutting nozzle 1 is fitted to the tapered fitting hole 2c of the piercing nozzle 2 with the clips 33 expanded by the removing member 34, and thereafter, the removing member 34 is removed from the clips.
  • the energizing force of the spring 32 acts on the pair of clips 32 to cause them to come close to each other, so that these clips 32 are kept fitted to the groove formed in the cutting nozzle 1.
  • the cutting nozzle 1 and the combination of the piercing nozzle 2 with the underlay 3 are connected together in one body through the attaching mechanism.
  • the removing member 34 is firstly pushed against the ends of the clips 33 to expand the clips 33 as shown by the broken line of Fig. 5. Thereupon, since the clips 33 are slipped out of the groove formed on the cutting nozzle 1, the piercing nozzle 2 and the underlay 3 connected thereto can be removed from the cutting nozzle 1.
  • the combination of the piercing nozzle 2 and the underlay 3 can be mounted to or detached from the cutting nozzle 1.
  • the combination of the piercing nozzle 2 and the underlay 3 may be kept always mounted to the cutting nozzle 1 or a machining head, for mounting the cutting nozzle 1 in a manner such that the combination can move relative to the cutting nozzle 1.
  • a mounting tool (not shown) is attached to the laser-beam machining head which mounts the cutting nozzle 1 so that it can move relative to the cutting nozzle 1, and then the combination of the piercing nozzle 2 and the underlay 3 is mounted to the mounting tool.
  • the mounting tool is operated to selectively place the combination of the piercing nozzle 2 and the underlay 3 at a position where the piercing nozzle 2 comes into engagement with the cutting nozzle 1 (during piercing works) and a position where the piercing nozzle 2 is placed distant from the cutting nozzle 1 (during normal cutting).
  • the following table 1 shows the results of experiment made under the conditions that a carbon dioxide gas laser oscillator of 3kW was used to carry out piercing for a mild steel sheet having a thickness of 25 mm through the injection of oxygen assist gas.
  • Piercing based on pulse output Piercing by means of cutting nozzle based on continuous output
  • Piercing according to the invention (based on continuous output)
  • (a) (b) Nozzle hole diameter (mm) 3.0 1.5 3.0 1.5
  • Assist gas pressure (kgf/cm 2 ) 0.3 1.0 0.3 1.0 Oscillator power (kW) 3 3 3 3 3 3
  • the piercing in the experiment (b) was carried out under the same conditions as the experiment (a), except that a nozzle having a hole diameter of 1.5 mm was used, and the pressure of the assist gas was set to 1.0 kgf/cm 2 . As a result, a piercing hole having a diameter of 1.5 mm was produced in 25 seconds.
  • the piercing was carried out under the conditions where a cutting nozzle having a hole diameter of 3.0 mm was used, the pressure of the assist gas was set to 0.3 kgf/cm 2 and the power of the laser oscillator was set to 3kW at its maximum based on continuous output. As a result, the piercing was completed in 3 seconds, while the diameter of a machined hole was as large as 20 to 30 mm.
  • the piercing was carried out under the conditions that a nozzle having a hole diameter of 1.5 mm was used, the pressure of the assist gas was set to 1.0 kgf/cm 2 and the power of the laser oscillator was set to 3kW at its maximum based on a continuous output. As a result, a piercing hole having a diameter of 6 mm was produced in 0.8 seconds.
  • the piercing according to the invention enables a hole having a smaller diameter to be formed in a shorter machining time, as compared with piercing by means of the cutting nozzle.
  • the piercing according to the invention when the piercing according to the invention is compared with the conventional piercing based on pulse output, it is found that a hole of a smaller diameter can be machined by the conventional piercing based on pulse output, while the machining time can be remarkably shortened by the piercing according to the invention.
  • the fact that the machining time for piercing is remarkably as short as 0.8 seconds in the case of the invention as shown in the table 1 results in that the time required for conduction of heat, which is produced when the machining target at the piercing position is melted by the laser beam 10, to the other area is remarkably shortened. For that reason, it is supposed that a piercing hole having a diameter of 6 mm, not so large, can be formed.
  • the table 2 shows the results of the experiment applied to a mild steel sheet (SS400 material) having a thickness of 19 mm by the use of a carbon dioxide gas laser oscillator of 3kW.
  • the table 3 shows the results of the experiment applied to a soft steel sheet (SS400 material) having a thickness of 25 mm by the use of a carbon dioxide gas laser oscillator of 6kW.
  • the machining was carried out with the assist gas pressure of 1.0 kgf/cm 2 and based on continuous output of laser oscillator. Since the machining time for piercing and the hole diameter are subject to variation, the numerical values in the tables 2 and 3 are given as their mean values.
  • the nozzle for piercing should have a hole diameter larger than the diameter of converged laser beam but not exceeding about 2.5 mm. Further, as is apparent from the tables 2 and 3, when the nozzle having a hole diameter in the range from 1.5 to 2.5 mm is in use, the machining time for piercing is below 1 second, and the diameter of a machined hole is in the range from 6 to 10 mm.
  • the machining time for piercing is largely subject to variation from below 1 ( ⁇ 1) to 3 seconds (the diameter of a machined hole is also subject to variation from 6 to 4 mm).
  • a nozzle having a hole diameter of about 1.5 mm is suitable for the piercing.
  • piercing may be carried out only by using the piercing nozzle without the need for an underlay.
  • the piercing in this case inevitably has a defect in that the dross is adhered to the surface of the machining target, while there is an advantage in that the piercing may be carried out for a short period of time.
  • dross is small in quantity, with the result that adhesion of the dross to the machining target is advantageously small.
  • the piercing may be carried out only by using the underlay 3 without the need for the piercing nozzle 2.
  • the piercing by using only the underlay may be applied to the conventional piercing to advantageously prevent the dross from adhering to the surface of the machining target.
  • a laser-beam machining device having an automatic nozzle exchanging device capable of automatically exchanging a nozzle mounted to the laser-beam machining head may be used for the piercing.
  • a cutting nozzle and a piercing nozzle are placed in advance in the automatic nozzle exchanging device.
  • the piercing nozzle is automatically mounted to the laser-beam machining head according to a command from a control device such as a numerical control unit operated by the input of an NC program.
  • the cutting nozzle is automatically mounted to the laser-beam machining head.
  • piercing may be carried out for a short period of time to machine a hole having a small diameter, and the quantity of scattered dross is decreased.
  • the underlay may be used to catch the scattered dross to prevent the dross from adhering to the surface of the machining target. Further, the scattered dross dropped down to the underlay may be forcibly removed to enable continuous piercing.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • Laser Beam Processing (AREA)

Abstract

A piercing nozzle (2) having a nozzle hole (2a) larger than the diameter of a converged laser beam (10) and smaller than the diameter of a hole (1a) of a cutting nozzle (1) is in use. Further, an underlay (3) having a hole (3a) at a position corresponding to the nozzle hole (2a) is placed under the piercing nozzle (2) with a clearance (5). Piercing is carried out by irradiating the laser beam (10) to a machining target (6) through nozzle holes (1a, 2a) and (3a) on condition that a laser oscillator is set to output high power. The diameter of a hole machined by the piercing is small, and less scattered dross is produced. The scattered dross is cooled down within the clearance (5) and is then dropped down to the underlay (3), so that the adhesion of the scattered dross to the machining target does not occur. Since a small hole is machined with the high power, the machining time for piercing is remarkably shortened.

Description

This invention relates to a laser-beam machining method, a laser-beam machining device, and an auxiliary tool, for carrying out machining to pierce a cutting target such as a steel sheet.
In a laser-beam machining method of cutting a machining target such as a steel sheet by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a nozzle having a small hole, piercing work or boring work is required at the start of machining.
A serious problem faced during piercing is the presence of scattered dross. Since boring of a machining target such as steel sheet or the like is carried out by melting the machining target by laser beam while jetting assist gas through the nozzle, scattering of dross resulting from melting the machining target by the laser beam occurs due to the assist gas jetted through the nozzle. There is a danger that the scattered dross may be adhered to the nozzle to damage the nozzle or be adhered to an operator to burn the operator. Further, the scattered dross adhered to the surface of the machining target hinders the subsequent machining for the machining target.
For preventing a nozzle from being damaged due to the scattered dross, there are known methods such as a method of making a nozzle of a metal of a high melting point material and that of placing a nozzle largely apart from a machining target only at the time of piercing (See Japanese Patent Applications Laid-open Nos. 63-52792 and 4-200891).
In addition, for the purpose of ensuring the safety of an operator, there are known methods such as a method of covering a machining point to prevent the dross from being scattered at the time of piercing and that of controlling the scattering direction of dross (See Japanese Patent Applications Laid-open Nos. 9-136177, 10-137970, 6-142972 and 10-225787).
However according to the above methods, the scattered dross is adhered to the surface of the machining target, resulting in the hindrance of the subsequent cutting. In this connection, for the purpose of preventing the scattered dross from adhering to the surface of the machining target, there is disclosed a method of shielding a machining point to collect the dross in Japanese Patent Application Laid-open No. 9-271980. However, this method is supposed to be used in association with piercing based on pulse output which is determined in advance in terms of such size and quantity of scattered dross as will enable the scattered dross to be absorbed and collected (See Japanese Patent Application Laid-open No. 5-185261).
Recently, an improvement on a laser oscillator for higher power has been made, and such improvement brings about a tendency toward increasing of the thickness of a steel sheet serving as a machining target. When such a steel sheet of a large thickness is subjected to piercing based on pulse output as described above, there is a problem in that it takes a long time to carry out the piercing. On the contrary, if piercing is carried out with laser power of continuous output, as in the case of normal cutting, and also at its maximum level, the piercing can be completed quickly. However, in this case, a large quantity of dross will be produced disadvantageously, resulting in the occurrence of adhesion of such dross in the shape of a lump to the surface of the machining target. On the other hand, if piercing is carried out with laser power of low continuous output, it will take a long time to carry out the piercing and adhesion will occur disadvantageously.
An object of the present invention is to provide a laser-beam machining method, a laser-beam machining device and an auxiliary tool for piercing which permit piercing at high speed.
Another object of the present invention is to provide a laser-beam machining method, a laser-beam machining device and an auxiliary tool for piercing which may reduce scattered dross, resulting in less occurrence of adhesion of the dross to a machining target.
Aspects of the present invention are provided by attached claims 1, 2, 4, 5, 7 and 10.
According to another aspect of the present invention, a nozzle having a hole diameter larger than a converged laser beam diameter and smaller than a hole diameter of a cuffing nozzle is used as a piercing nozzle. The nozzle has a hole diameter preferably, but not essentially, of not more than 2.5 mm.
Piercing may be carried out on condition that an underlay formed by a metal sheet having a hole therein, possibly in the center, is placed on the machining target, so that the underlay is permitted to catch the scattered dross so as to avoid the dross from adhering to the surface of the machining target.
A piercing nozzle may be connected to the tip of a cutting nozzle at the time of piercing, for the reason that piercing carried out using a cutting or piercing nozzle having a relatively small hole diameter may shorten the time taken for the piercing and may cause less scattering of the dross, in comparison with the piercing carried out using a cutting nozzle having a relatively large hole diameter. In addition, the piercing nozzle may be mounted to the cutting nozzle detachably, or may be mounted to be movable between a piercing position and a shunting position.
A clearance for cooling down the scattered dross may be provided between the piercing nozzle and an underlay. There may also be provided a blade driven in the clearance to remove the scattered dross from the surface of the underlay, and/or a scattered dross removing means to remove the scattered dross by flowing gas or a fluid into the clearance.
Further, the piercing nozzle added to the cuffing nozzle, and the underlay, may be provided in a pair as an auxiliary tool for piercing.
The foregoing and other features will become apparent from the following description of preferred embodiments of the invention with reference to the accompanying drawings, in which:
  • Fig. 1 is a sectional view showing a basic part of a nozzle portion of a laser-beam machining device according to a first embodiment of the present invention, in which a combination of a piercing nozzle and an underlay is joined to a cuffing nozzle;
  • Fig. 2A is a view showing the laser-beam machining device of Fig. 1, which is carrying out piercing;
  • Fig. 2B is a view showing the cuffing nozzle of Fig. 2A which is carrying out normal cuffing for a target, with the piercing nozzle and the underlay removed from the laser-beam machining device of Fig. 2A;
  • Fig. 3A is a sectional view showing a basic part of a nozzle portion of a laser-beam machining device according to a second embodiment of the present invention, in which a combination of a piercing nozzle and an underlay is joined to a cutting nozzle;
  • Fig. 3B is a view showing the piercing nozzle of Fig. 3A, as viewed from the bottom, after the removal of the underlay placed below the piercing nozzle;
  • Fig. 4A is a sectional view showing a basic part of a nozzle portion of a laser-beam machining device according to a third embodiment of the present invention, in which a combination of a piercing nozzle and an underlay is joined to a cutting nozzle;
  • Fig. 4B is a view showing the piercing nozzle of Fig. 4A, as viewed from the bottom, after the removal of the underlay placed below the piercing nozzle; and
  • Fig. 5 is a view for explaining a mounting mechanism provided on a laser-beam machining device according to a fourth embodiment of the present invention to detachably mount a piercing nozzle and an underlay to a cutting nozzle.
  • A description will now be given of a laser-beam machining device according to the first embodiment of the present invention with reference to Fig. 1.
    The laser-beam machining device comprises a cutting nozzle 1 normally used for cutting a machining target and a piercing nozzle 2 used in combination with the cutting nozzle 1 for piercing. Further, a pivotal portion 4 is provided on one end of the piercing nozzle 2, and an underlay 3 is mounted to the piercing nozzle 2 through the pivotal portion 4 so that it can rotate relative to and can be detached from the piercing nozzle 2.
    Further, a spacer 2b is provided in a projected state at four corners of the lower surface (i.e., the surface opposite to the surface brought into engagement with the cutting nozzle 1) of the piercing nozzle 2, so that when the underlay 3 is placed on the side of the piercing nozzle 2, a clearance 5 is formed between the piercing nozzle 2 and the underlay 3, as shown in Fig. 1.
    The underlay 3 is used to prevent scattered dross from adhering to the surface of a machining target 6 at the time of piercing. The underlay 3 has a hole 3a in the center. When carrying out piercing, the underlay 3 is placed in a manner such that the hole 3a and a hole 2a of the piercing nozzle 2 overlap with each other, in particular, in a manner such that the center of the hole 3a of the underlay 3 is placed in alignment with the center of the hole 2a of the piercing nozzle 2.
    The upper surface of the piercing nozzle 2 has a tapered fitting hole 2c, to which the tip of the cutting nozzle 1 is capable of being fitted. The tip of the cutting nozzle 1 has a nozzle hole 1a in the center. Further, the piercing hole 2a is formed to extend from the center of the tapered fitting hole 2c to the lower surface of the piercing nozzle 2.
    Thus, when the tip of the cutting nozzle 1 is fitted to the tapered fitting hole 2c of the piercing nozzle 2, the center of the nozzle hole 1a at the tip of the cutting nozzle 1, the center of the piercing hole 2a and the center of the hole 3a of the underlay 3 are placed in alignment with a common aids, as shown in Fig. 1.
    When carrying out piercing for the machining target 6, a laser beam 10 passes through the nozzle hole 1a at the tip of the cutting nozzle 1, the piercing hole 2a and the hole 3a of the underlay 3 and then reaches the machining target 6.
    The underlay 3 needs to have a size enough to cover the scattering range of the dross caused by the piercing. In this embodiment, a flat sheet in the shape of a square of 60 mm x 60 mm with a thickness of 3 mm is in use, and its material is the same copper alloy as the piercing nozzle 2.
    Further, if the hole 3a formed in the underlay 3 is too large, the scattered dross will adhere to the surface of the machining target 6 at a portion corresponding to the hole 3a, and therefore, it is better to form the hole 3a as small as possible. However, if the hole 3a is too small, it will take a longer time disadvantageously to carry out piercing on account of reduction in an area of the part of machining target 6 where the assist gas 11 strikes, and so on.
    Thus, a suitable size of the hole 3a of the underlay 3, which is larger than the hole 2a of the piercing nozzle 2, is found by an experiment or the like. According to this embodiment, since the diameter of the hole 2a of the piercing nozzle 2 is set to 1.5 mm as will be described later, the hole 3a of the underlay 3 is formed to have a diameter of about 5 mm. Further, the clearance 5 between the underlay 3 and the piercing nozzle 2 is set to 3 mm.
    Since the piercing nozzle 2 is used for catching scattered dross above the underlay 3, its size is set to be substantially equal to that of the underlay 3.
    Further, the nozzle hole 2a of the piercing nozzle 2 is formed to be smaller in diameter than the nozzle hole 1a of the cutting nozzle 1. If the nozzle hole 2a has a larger diameter, an area of the part of machining target 6 where the assist gas 11 jetted through the nozzle hole 2a strikes is increased and injection speed of the assist gas is reduced, in comparison with the case where the nozzle hole 2a has a smaller diameter with the assist gas 20 supplied under the same pressure. Thus, if diameter of the nozzle hole 2a is increased, the force for scattering the dross of the machining target melted in the process of piercing is reduced, bringing about a delay of scattering, with the result that the diameter of a hole formed by piercing increases and scattered dross increases in quantity.
    On the other hand, if the nozzle hole 2a has a smaller diameter, the injection speed is increased and an area of the part of machining target 6 where the assist gas 11 strikes is reduced, in comparison with the case where the nozzle hole 2a has a larger diameter with the assist gas 11 supplied under the same pressure. Thus, if diameter of the nozzle hole 2a is decreased, the force for scattering the dross of the machining target melted in the process of piercing is increased, bringing about quick scattering of the dross caused by the irradiation of the laser beam 10, with the result that the diameter of a hole machined by the piercing decreases and scattered dross decreases in quantity.
    In view of the above, the nozzle hole 2a of the piercing nozzle 2 preferably needs to have a diameter larger than the diameter of converged laser beam 10 and smaller than the nozzle hole 1a of the cutting nozzle 1.
    In this connection, according to this embodiment, since the nozzle hole 1a of the cutting nozzle 1 has a diameter of 4 mm, and the laser beam 10 has a converged spot diameter of about 0.8 mm, the nozzle hole 2a of the piercing nozzle 2 is formed to have a diameter of 1.5 mm (larger than 0.8 mm and smaller than 4 mm). Further, the length of the hole 2a of the piercing nozzle 2, which has diameter of 1.5 mm, is set to 10 mm. In piercing using this piercing nozzle 2, it is ascertained that it does not matter if the laser beam is reflected from the inner wall of the piercing nozzle 2.
    A description will now be given of the operation to carry out the machining to pierce the machining target by using the laser-beam machining device according to this embodiment.
    First, the cutting nozzle 1 is put above a target position for machining to pierce the machining target 6. Subsequently, the tapered fitting hole 2c of the piercing nozzle 2 is fitted to the tip of the cutting nozzle 1 to combine the cutting nozzle 1 with the piercing nozzle 2 and the underlay 3. Then, the cutting nozzle 1, the piercing nozzle 2 and the underlay 3 are moved down in a combined state toward a piercing position on the machining target 6 such that the underlay 3 is placed on the surface of the machining target 6 as shown in Fig. 1.
    After the completion of the positioning described above, the laser oscillator (not shown) is activated to irradiate the converged laser beam 10 to the machining target 6 through the hole 1a of the cutting nozzle 1, the hole 2a of the piercing nozzle 2 and the hole 3a of the underlay 3 (see Fig. 2A), while the injection of the assist gas 11 to the machining target 6 is carried out through the holes 1a, 2a and 3a. Thereupon, , the portion of the machining target 6, irradiated by the laser beam 10, starts melting. Then, the resultant dross is removed from the machining target 6 by high-speed and high-pressure assist gas 11 jetted through the small-diameter nozzle hole 2a of the piercing nozzle 2.
    On the other hand, the assist gas 11 is turned in a reverse direction after striking against the machining target 6 and is then exhausted from the hole 3a of the underlay 3 to the outside through the clearance 5 between the piercing nozzle 2 and the underlay 3, while the dross carried by the assist gas 11 is cooled down in the course of the passage through the clearance 5 and is then dropped down to the underlay 3, resulting in the adhesion of the dross to the underlay 3.
    As described above, according to the embodiment, since the assist gas 11 is jetted at high speed under high pressure to a narrow area of the machining target 6 through the small nozzle hole 2a of the piercing nozzle 2, the dross is removed from the machining target 6 at high speed, so that the laser beam 10 is allowed to melt the inner part of the machining target 6. As a result, with an increase in machining speed for piercing, a hole machined by the piercing decreases in diameter, and the scattered dross also decreases in quantity.
    After the completion of the piercing as described above, the piercing nozzle 2 and the underlay 3 are removed from the cutting nozzle 1 to start the normal cutting with the cutting nozzle 1 (refer to Fig. 2B).
    On the other hand, the piercing nozzle 2 and the underlay 3, having been removed from the cutting nozzle 1, is put in a ready state for the next piercing after opening the piercing nozzle 2 through the pivotal motion relative to the underlay 3 about the pivotal portion 4 or separating the underlay 3 from the piercing nozzle 2 and then scraping off the adhered dross from the underlay 3.
    A description will now be given of a laser-beam machining device according to the second embodiment of the present invention with reference to Figs. 3A and 3B.
    According to the second embodiment, a cover 2b' is formed at the edge of the piercing nozzle 2, so that when the piercing nozzle 2 is placed opposite to the underlay 3, the cover 2b' serves as a spacer to form a clearance 5 of a predetermined depth between the piercing nozzle 2 and the underlay 3, and also to define the sectional shape of the clearance 5.
    Fig. 3B is a view showing the piercing nozzle 2 of Fig. 3A as viewed from the bottom, after the removal of the underlay 3 placed below the piercing nozzle 2. As shown in Fig. 3B, the clearance 5 has a substantially circular sectional shape. The cover 2b' has three paths (a path leading to an exhaust port 21, a path leading to an inlet port 22 and a path leading to an injection port 23) which are formed in a parallel arrangement to permit the communication between the clearance 5 and the outside of the piercing nozzle 2.
    The assist gas 11 in the clearance 5 is exhausted to the outside through the exhaust port 21. A fluid such as compressed air is supplied from the outside into the clearance 5 through the inlet port 22. Oil, a soap solution or a surface active solution is jetted or sprayed from the outside into the clearance 5 through the injection port 23.
    When carrying out piercing, the compressed air supplied into the clearance 5 through the inlet port 22 flows along the inner surface of the clearance 5 of the circular sectional shape to form a swirl flow and is then exhausted through the exhaust port 21. In this process, the dross scattered by the assist gas 11 is cooled down by the compressed air and is then exhausted through the exhaust port 21. Since the dross is cooled down by the compressed air before being exhausted through the exhaust port 21 as described above, the quantity of dross adhered to the surface of the underlay 3, which is exhausted through the exhaust port 21 and then dropped down to the underlay 3, is decreased. Incidentally, a fluid (gas or liquid) other than the compressed air may be supplied through the inlet port 22.
    Further, since the scattered dross is covered and then cooled down with oil, soap solution or surface active solution which has been jetted into the clearance 5 through the injection port 23, the dross dropped down to the underlay 3 after having been cooled down is hardly adhered to the underlay 3, and as a result, is exhausted through the exhaust port 21 together with the compressed air supplied through the inlet port 22.
    In consequence, the piercing nozzle 2 and the underlay 3 may be used for a long time without being cared for. Further, even if the dross is adhered to the underlay 3, it is possible to easily remove the adhered dross from the underlay 3 by enclosing the adhered dross with the oil, the soap solution or the surface active solution.
    As described above, according to the second embodiment, since the scattered dross in the clearance 5 is cooled down by the compressed air and also by oil, soap solution or surface active solution and is thereafter exhausted through the exhaust port 21 while being carried on the swirl flow of the compressed air, the scattered dross seldom continue to accumulate in the clearance 5. Thus, the laser-beam machining device according to the second embodiment may carry out the piercing continuously without frequent operation for removing the dross.
    A description will now be given of a laser-beam machining device according to the third embodiment with reference to Figs. 4A and 4B.
    The laser-beam machining device according to the third embodiment is equivalent to a laser-beam machining device having a plurality of blades 24 (six blades in the embodiment shown in Fig. 4B) provided in a rotatable state in the clearance 5 of the laser-beam machining device according to the second embodiment.
    These blades 24 are mounted on the piercing nozzle 2 at the center portion thereof (a portion surrounding the nozzle hole 2a) through a ball bearing 25 so that they can rotate. More specifically, as shown in Fig. 4A, a cylindrical projection projecting toward the clearance 5 is formed in the center of the piercing nozzle 2, and an inner race of the ball bearing 25 is fixed to the projection. On the other hand, these six blades 24 are fixed to the outer race of the ball bearing 25.
    These blades 24 are rotated by the compressed air supplied into the clearance 5 through the inlet port 22 in the course of piercing. Thus, dross caused by irradiation of the laser beam 10 and then scattered by the assist gas 11 is carried toward the exhaust port 21 together with the assist gas through the rotation of the blades 24 while being cooled down by the compressed air and is then exhausted through the exhaust port 21. Further, even if the dross dropped down to the underlay 3 tends to be adhered thereto, the rotating blades 24 carry the dross toward the exhaust port 21 after having scraped off from the underlay 3, and the dross is exhausted through the exhaust port 21.
    As described above, when carrying out piercing using the laser-beam machining device according to the third embodiment, since the dross is forcibly exhausted by the blades 24, the dross can not accumulate in the clearance 5, so that it is possible to carry out piercing continuously. Further, since the dross is not allowed to adhere and accumulate on the underlay 3, there is no need to frequently clean the underlay 3.
    In the laser-beam machining device according to the second embodiment, the underlay 3 and the piercing nozzle 2 are connected together pivotally through the pivotal means (the pivotal portion 4). In the laser-beam machining device according to the third embodiment, a fixing means such as a set screw is used to connect the underlay 3 and the piercing nozzle 2 together.
    In the laser-beam machining device according to the third embodiment as described above, the compressed air is supplied into the clearance 5 through the inlet port 22. But as a modification of the third embodiment, fluid such as compressed air need not be supplied through the inlet port 22, or the inlet port 22 for supplying the fluid need not be formed in the cover 2b' of the piercing nozzle 2.
    According to the above modification, the assist gas 11 jetted at high speed under high pressure toward the machining target 6 is turned in the reverse direction after striking against the machining target 6 and then flows into the clearance 5 between the piercing nozzle 2 and the underlay 3, while the assist gas 11 in the clearance 5 forms a swirl flow and is then exhausted to the outside through the exhaust port 21 serving as the only outlet. The swirl flow of the assist gas 11 causes the rotation of the blades 24. Thus, even in this modification, since the dross adhered to the underlay 3 may be scraped off from the underlay through the rotation of the blades 24, the laser-beam machining device according to this modification may display the substantially similar functions to those of the laser-beam machining device according to the third embodiment shown in Figs. 4A and 4B.
    In any of laser-beam machining device according to the first, second and third embodiments, connection of the piercing nozzle 2 to the cutting nozzle 1 is carried out only by fitting the tip of the cutting nozzle 1 to the tapered fitting hole 2a of the piercing nozzle 2 without any special attaching mechanism used.
    A description will now be given of a laser-beam machining device having an attaching mechanism which is used for mounting a combination of the piercing nozzle 2 and the underlay 3 on the cutting nozzle 1, as the fourth embodiment, with reference to Fig. 5. Fig. 5 is a view of the cutting nozzle 1 mounted with the piercing nozzle 2 though the attaching mechanism, as viewed from the top. It should be noted that the piercing nozzle 2 mounted with the attaching mechanism as will be described later and the underlay 3 connected to this piercing nozzle 2 have the same structure as those of the laser-beam machining device according to the first, second and third embodiments.
    The outer surface of the cutting nozzle 1 has a groove to which a pair of clips 33 (which will be described later) constituting a mounting mechanism are fitted.
    On the other hand, a pair of shafts 31 are provided in a projected state on one side of the upper surface (i.e., the surface on the side opposite to the cutting nozzle 1) of the piercing nozzle 2, and the bases of the clips 33 are respectively mounted to the shafts 31 in a pivotal state. Further, a spring 32 is provided between these two clips 33, and these two clips 33 are energized to come close to each other by means of the spring 32.
    Each clip 33 has a tapered end, and a distance between the inner edge of one clip 33 and the inner edge of the other clip 33 gradually widens toward the ends of the clips. Then, when a removing member 34 is pressed against the ends of the clips 33 and is then pushed toward the cutting nozzle 1, the pair of clips 33 are expanded against the force of the spring 32 as shown by a broken line of Fig. 5.
    The tip of the cutting nozzle 1 is fitted to the tapered fitting hole 2c of the piercing nozzle 2 with the clips 33 expanded by the removing member 34, and thereafter, the removing member 34 is removed from the clips. Thereupon, the energizing force of the spring 32 acts on the pair of clips 32 to cause them to come close to each other, so that these clips 32 are kept fitted to the groove formed in the cutting nozzle 1. As a result, the cutting nozzle 1 and the combination of the piercing nozzle 2 with the underlay 3 are connected together in one body through the attaching mechanism.
    In this connection, when an assembly of the cutting nozzle 1 and combination of the piercing nozzle 2 and the underlay 3, connected with each other through the attaching mechanism in one body, is moved to the piercing position, the cutting nozzle 1, the piercing nozzle 2 and the underlay 3 are simultaneously placed at the piercing position.
    In the case of starting normal cutting after completion of piercing, the removing member 34 is firstly pushed against the ends of the clips 33 to expand the clips 33 as shown by the broken line of Fig. 5. Thereupon, since the clips 33 are slipped out of the groove formed on the cutting nozzle 1, the piercing nozzle 2 and the underlay 3 connected thereto can be removed from the cutting nozzle 1.
    As described above, according to the fourth embodiment, the combination of the piercing nozzle 2 and the underlay 3 can be mounted to or detached from the cutting nozzle 1. However, as a modification of this embodiment, the combination of the piercing nozzle 2 and the underlay 3 may be kept always mounted to the cutting nozzle 1 or a machining head, for mounting the cutting nozzle 1 in a manner such that the combination can move relative to the cutting nozzle 1. For instance, a mounting tool (not shown) is attached to the laser-beam machining head which mounts the cutting nozzle 1 so that it can move relative to the cutting nozzle 1, and then the combination of the piercing nozzle 2 and the underlay 3 is mounted to the mounting tool. Then, the mounting tool is operated to selectively place the combination of the piercing nozzle 2 and the underlay 3 at a position where the piercing nozzle 2 comes into engagement with the cutting nozzle 1 (during piercing works) and a position where the piercing nozzle 2 is placed distant from the cutting nozzle 1 (during normal cutting).
    The following table 1 shows the results of experiment made under the conditions that a carbon dioxide gas laser oscillator of 3kW was used to carry out piercing for a mild steel sheet having a thickness of 25 mm through the injection of oxygen assist gas.
    Piercing based on pulse output Piercing by means of cutting nozzle (based on continuous output) Piercing according to the invention (based on continuous output)
    (a) (b)
    Nozzle hole diameter (mm) 3.0 1.5 3.0 1.5
    Assist gas pressure (kgf/cm2) 0.3 1.0 0.3 1.0
    Oscillator power (kW) 3 3 3 3
    Output frequency of oscillator (Hz) 10 10 - -
    Duty ratio (%) 30 30 100 100
    Machined hole diameter (mm) 1.5 1.5 20-30 6
    Machining time (sec) 30 25 3 0.8
    In the above table 1, according to "piercing based on pulse output" two kinds of experiments (a) and (b), different in nozzle hole diameter from each other, were made. The piercing in the experiment (a) was carried out under the conditions where a normal cutting nozzle having a hole diameter of 3.0 mm was used, and the pressure of assist gas was set to 0.3 kgf/cm2. The power of the laser oscillator was set to 3kW at its maximum, and the output frequency of the oscillator and the duty ratio were respectively set to 10 Hz and 30%. As the result of the piercing carried out under the above conditions, a piercing hole having a diameter of 1.5 mm was produced in the machining time of 30 seconds.
    On the other hand, the piercing in the experiment (b) was carried out under the same conditions as the experiment (a), except that a nozzle having a hole diameter of 1.5 mm was used, and the pressure of the assist gas was set to 1.0 kgf/cm2. As a result, a piercing hole having a diameter of 1.5 mm was produced in 25 seconds.
    In the experiment on "piercing by means of the cutting nozzle", the piercing was carried out under the conditions where a cutting nozzle having a hole diameter of 3.0 mm was used, the pressure of the assist gas was set to 0.3 kgf/cm2 and the power of the laser oscillator was set to 3kW at its maximum based on continuous output. As a result, the piercing was completed in 3 seconds, while the diameter of a machined hole was as large as 20 to 30 mm.
    In the experiment on "piercing according to the invention", the piercing was carried out under the conditions that a nozzle having a hole diameter of 1.5 mm was used, the pressure of the assist gas was set to 1.0 kgf/cm2 and the power of the laser oscillator was set to 3kW at its maximum based on a continuous output. As a result, a piercing hole having a diameter of 6 mm was produced in 0.8 seconds.
    As is apparent from the table 1, the piercing according to the invention enables a hole having a smaller diameter to be formed in a shorter machining time, as compared with piercing by means of the cutting nozzle.
    In addition, when the piercing according to the invention is compared with the conventional piercing based on pulse output, it is found that a hole of a smaller diameter can be machined by the conventional piercing based on pulse output, while the machining time can be remarkably shortened by the piercing according to the invention. In particular, the fact that the machining time for piercing is remarkably as short as 0.8 seconds in the case of the invention as shown in the table 1 results in that the time required for conduction of heat, which is produced when the machining target at the piercing position is melted by the laser beam 10, to the other area is remarkably shortened. For that reason, it is supposed that a piercing hole having a diameter of 6 mm, not so large, can be formed.
    The following tables 2 and 3 respectively show the results of the experiments when the cutting and the piercing were carried out with nozzles of various diameters.
    (Power of 3kw, SS400 material with thickness of 19mm)
    Nozzle diameter (mm) 0.5 1.0 1.5 2.0 2.5 3.0 4.0 5.0
    Cutting No good No good No good Defective, Adhesion of dross Defective, Defective in cutting plane Good Good No good
    Piercing (sec) 6 3 <1 <1 <1 <1 <1 <1
    Machined hole diameter (mm) 3 4 6 8 10 Defective Defective Defective
    (Power of 6kw, SS400 material with thickness of 25mm)
    Nozzle diameter (mm) 0.5 1.0 1.5 2.0 2.5 3.0 4.0 5.0
    Cutting Beam diameter is too large No good No good No good Defective, Adhesion of dross Defective, Defective in cutting plane Good Good
    Piercing (sec) 3 <1 <1 <1 <1 <1 <1
    Machined hole diameter (mm) 4 6 8 10 Defective Defective Defective
    The table 2 shows the results of the experiment applied to a mild steel sheet (SS400 material) having a thickness of 19 mm by the use of a carbon dioxide gas laser oscillator of 3kW. The table 3 shows the results of the experiment applied to a soft steel sheet (SS400 material) having a thickness of 25 mm by the use of a carbon dioxide gas laser oscillator of 6kW. The machining was carried out with the assist gas pressure of 1.0 kgf/cm2 and based on continuous output of laser oscillator. Since the machining time for piercing and the hole diameter are subject to variation, the numerical values in the tables 2 and 3 are given as their mean values.
    As is apparent from the above tables 2 and 3, the use of a nozzle having a hole diameter of not less than 3.0 mm results in defective piercing, for the reasons that the diameter of a machined hole is made too large, so that a large quantity of dross is scattered and is then adhered to the machining target, resulting in the hindrance of the subsequent cutting, and that a portion around the machining point is heated up to a high temperature to excess, so that the machining target is placed in an overheated state in the subsequent cutting to bring about the abnormal burning, that is, "self burning".
    In view of the above, it is to be desired that the nozzle for piercing should have a hole diameter larger than the diameter of converged laser beam but not exceeding about 2.5 mm. Further, as is apparent from the tables 2 and 3, when the nozzle having a hole diameter in the range from 1.5 to 2.5 mm is in use, the machining time for piercing is below 1 second, and the diameter of a machined hole is in the range from 6 to 10 mm.
    On the other hand, when the hole diameter of the nozzle is changed from 1.5 to 1.0 mm, the machining time for piercing is largely subject to variation from below 1 (<1) to 3 seconds (the diameter of a machined hole is also subject to variation from 6 to 4 mm).
    In view of the above, it may be said that a nozzle having a hole diameter of about 1.5 mm is suitable for the piercing.
    The above description has been given of the embodiments in which the piercing nozzle 2 and the underlay 3 are used in a pair, however, it is to be understood that piercing may be carried out only by using the piercing nozzle without the need for an underlay. The piercing in this case inevitably has a defect in that the dross is adhered to the surface of the machining target, while there is an advantage in that the piercing may be carried out for a short period of time. In addition, since a hole having a small diameter is machined by the piercing in this case, dross is small in quantity, with the result that adhesion of the dross to the machining target is advantageously small.
    On the other hand, the piercing may be carried out only by using the underlay 3 without the need for the piercing nozzle 2. In this case, the piercing by using only the underlay may be applied to the conventional piercing to advantageously prevent the dross from adhering to the surface of the machining target.
    Further, the above description has been given of the embodiments in which the piercing nozzle 2 is attached to the cutting nozzle 1, however, a laser-beam machining device having an automatic nozzle exchanging device capable of automatically exchanging a nozzle mounted to the laser-beam machining head may be used for the piercing. In this case, a cutting nozzle and a piercing nozzle are placed in advance in the automatic nozzle exchanging device. When carrying out the piercing, the piercing nozzle is automatically mounted to the laser-beam machining head according to a command from a control device such as a numerical control unit operated by the input of an NC program. And after completion of the piercing, the cutting nozzle is automatically mounted to the laser-beam machining head.
    As described above,
    piercing may be carried out for a short period of time to machine a hole having a small diameter, and the quantity of scattered dross is decreased. The underlay may be used to catch the scattered dross to prevent the dross from adhering to the surface of the machining target. Further, the scattered dross dropped down to the underlay may be forcibly removed to enable continuous piercing.

    Claims (14)

    1. A laser-beam machining method of carrying out machining to pierce or cut a machining target by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a hole of a machining nozzle mounted to a machining head, and simultaneously jetting assist gas through the hole of said nozzle, comprising the steps of:
      carrying out machining by using a cutting nozzle as said machining nozzle at the time of cutting; and
      carrying out piercing by using a piercing nozzle as said machining nozzle at the time of piercing, said piercing nozzle having a hole diameter larger than a converged laser beam diameter but smaller than a hole diameter of said cutting nozzle and being positioned in place of said cutting nozzle or being mounted onto the tip of said cutting nozzle.
    2. A laser-beam machining method of carrying out machining to pierce a machining target by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a hole of a machining nozzle mounted to a machining head, and simultaneously jetting assist gas through the hole of said nozzle, comprising the step of:
      carrying out the piercing under the circumstance where an underlay formed by a metal sheet having a hole is placed on the machining target such that a piercing point and the hole of said underlay overlap with each other.
    3. A laser-beam machining method according to claim 1, wherein the piercing is carried out under the circumstance where an underlay formed by a metal sheet having a hole is placed on the machining target such that a piercing point and the hole of said underlay overlap with each other.
    4. A laser-beam machining device including an automatic nozzle exchanging means for automatically exchanging a nozzle to be mounted to a mounting head for carrying out machining to pierce or cut a machining target by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a nozzle hole, and simultaneously jetting assist gas through said nozzle hole, comprising:
      a cutting nozzle; and
      a piercing nozzle having a hole diameter
      which is larger than a converged laser beam diameter but smaller than a hole diameter of said cutting nozzle;
      wherein the piercing is carried out by mounting said piercing nozzle to the machining head by means of said automatic nozzle exchanging means at the time of piercing.
    5. A laser-beam machining device for machining a machining target by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a hole of a nozzle, and simultaneously jetting assist gas through the hole of said nozzle, comprising:
      an underlay applied to piercing to cover the machining target;
      wherein said underlay is combined with said nozzle at the time of piercing such that a hole provided in said underlay and the hole of said nozzle overlap with each other.
    6. A laser-beam machining device according to claim 4, wherein it further comprises an underlay formed by a metal sheet having a hole, and said underlay is combined with said piercing nozzle at the time of piercing such that the center of the hole of said underlay is in alignment with the center of the hole of said piercing nozzle.
    7. A laser-beam machining device for carrying out machining to pierce or cut a machining target by irradiating a laser beam outputted from a laser oscillator to the machining target in a converged state through a nozzle hole, and simultaneously jetting assist gas through said nozzle hole, comprising:
      a piercing nozzle detachably mounted to a cutting nozzle or mounted to be movable between a piercing position and a retreat position;
      wherein a hole dimeter of said piercing nozzle is larger than a converged laser beam diameter and is smaller than a hole diameter of said cutting nozzle.
    8. A laser-beam machining device according to claim 7, wherein it further comprises an underlay formed by a metal sheet having a hole and mounted to said piercing nozzle, and said underlay is placed at the time of piercing such that the hole of said underlay and the hole of said piercing nozzle overlap with each other.
    9. A laser-beam machining device according to any one of claims 5, 6 and 8, wherein a clearance is provided between said piercing nozzle and said underlay.
    10. An auxiliary tool for piercing, comprising:
      a piercing nozzle having a hole diameter smaller than the hole diameter of a cutting nozzle; and
      an underlay mounted to said piercing nozzle with a clearance;
      wherein said underlay has a hole which overlaps with the hole of said piercing nozzle.
    11. A laser-beam machining device according to claim 9, or an auxiliary tool according to claim 10, which further comprises a scattered dross removing means operable in said clearance to remove scattered dross from said underlay.
    12. A laser-beam machining device, or an auxiliary tool, according to claim 11, wherein said scattered dross removing means includes a means for jetting gas or a fluid into said clearance and/or a blade rotatable within said clearance.
    13. A laser-beam machining method according to any one of claims 1 to 3, or a laser-beam machining device or an auxiliary tool according to any one of claims 4 to 12, wherein the hole diameter of the piercing nozzle is 2.5 mm or less.
    14. A laser-beam machining method or device, or an auxiliary tool for piercing, wherein a nozzle having a hole diameter larger than a converged laser-beam diameter, and smaller than a hold diameter of a cutting nozzle, is used as a piercing nozzle.
    EP99307625A 1998-10-21 1999-09-28 Laser-beam machining method, laser-beam machining device and auxiliary tool for piercing Withdrawn EP1005945A3 (en)

    Applications Claiming Priority (2)

    Application Number Priority Date Filing Date Title
    JP31834498A JP3198095B2 (en) 1998-10-21 1998-10-21 Laser processing equipment
    JP31834498 1998-10-21

    Publications (2)

    Publication Number Publication Date
    EP1005945A2 true EP1005945A2 (en) 2000-06-07
    EP1005945A3 EP1005945A3 (en) 2004-05-12

    Family

    ID=18098121

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP99307625A Withdrawn EP1005945A3 (en) 1998-10-21 1999-09-28 Laser-beam machining method, laser-beam machining device and auxiliary tool for piercing

    Country Status (3)

    Country Link
    US (2) US6335507B1 (en)
    EP (1) EP1005945A3 (en)
    JP (1) JP3198095B2 (en)

    Cited By (2)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    EP1145796A1 (en) * 2000-04-10 2001-10-17 Tanaka Engineering Works, Ltd. Piercing device for laser cutter
    DE102006040784B4 (en) * 2005-09-07 2015-06-25 Disco Corp. Laser beam processing machine

    Families Citing this family (14)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    JP3198095B2 (en) * 1998-10-21 2001-08-13 ファナック株式会社 Laser processing equipment
    JP3714931B2 (en) * 2002-12-12 2005-11-09 コマツ産機株式会社 Plasma cutting method and apparatus
    US6969822B2 (en) * 2003-05-13 2005-11-29 Hewlett-Packard Development Company, L.P. Laser micromachining systems
    US7619180B2 (en) * 2003-06-25 2009-11-17 Reinhard Diem Laser head of a laser beam processing machine comprising alternating nozzles
    DE50312360D1 (en) * 2003-08-09 2010-03-11 Trumpf Werkzeugmaschinen Gmbh Laser processing nozzle coupling
    DE102004041273A1 (en) * 2004-08-23 2006-03-02 Alstom Technology Ltd drilling
    JP4720380B2 (en) * 2005-08-31 2011-07-13 澁谷工業株式会社 Laser processing equipment
    EP2189236B1 (en) * 2008-11-21 2012-06-20 Synova S.A. Method and apparatus for improving reliability of a machining process
    US8829388B2 (en) * 2011-07-29 2014-09-09 Ipg Photonics Corporation Method for contactless laser welding and apparatus
    CN105108337B (en) * 2015-09-01 2017-07-28 广东工业大学 A kind of turbine blade method for repairing crack
    KR101886822B1 (en) * 2016-12-07 2018-08-08 홍준화 Reparing method for soundproofing panel and repairing system for soundproofing panel
    JP6577110B2 (en) * 2017-10-06 2019-09-18 株式会社アマダホールディングス Laser processing method and laser processing apparatus
    CN114871602B (en) * 2022-04-19 2024-08-30 济南金威刻激光科技股份有限公司 Pipe supporting device for all-round laser cutting machine
    US12472580B2 (en) * 2022-06-01 2025-11-18 Caterpillar Inc. Laser handheld trimming and welding device

    Family Cites Families (25)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US3597578A (en) * 1967-03-16 1971-08-03 Nat Res Dev Thermal cutting apparatus and method
    JPS62158593A (en) 1985-12-28 1987-07-14 Murata Mach Ltd Laser beam machine
    JPS6352792A (en) 1986-08-21 1988-03-05 Mitsubishi Electric Corp Laser processing equipment
    JPH02284780A (en) 1989-04-27 1990-11-22 Amada Co Ltd Pierce forming method in laser beam machining and laser beam nozzle device
    JP2618730B2 (en) * 1990-01-29 1997-06-11 松下電器産業株式会社 Laser processing method and laser processing apparatus
    JP2856854B2 (en) 1990-07-11 1999-02-10 日本放送協会 Solid-state imaging device
    JP2875626B2 (en) 1990-11-30 1999-03-31 小池酸素工業株式会社 Laser piercing method
    JPH05185261A (en) 1991-03-07 1993-07-27 Fanuc Ltd Method for controlling piercing in laser beam machine
    JPH05111783A (en) * 1991-10-19 1993-05-07 Fanuc Ltd Drilling method for laser beam machining
    TW270907B (en) * 1992-10-23 1996-02-21 Mitsubishi Electric Machine
    JP3179892B2 (en) 1992-10-28 2001-06-25 日立建機株式会社 Laser processing apparatus and laser processing method
    JP2720744B2 (en) * 1992-12-28 1998-03-04 三菱電機株式会社 Laser processing machine
    JPH07223084A (en) * 1994-02-10 1995-08-22 Fanuc Ltd Laser beams machining device
    JPH09136177A (en) 1995-11-10 1997-05-27 Fuji Electric Co Ltd Laser processing equipment
    JP3526998B2 (en) 1996-01-18 2004-05-17 株式会社アマダ Laser processing method for surface coating material and laser processing head used for the same
    JPH09271980A (en) 1996-04-08 1997-10-21 Amada Co Ltd Method and device for sucking spatter and the like in laser beam machine
    JPH10113784A (en) 1996-10-08 1998-05-06 Amada Co Ltd Laser beam machine
    JPH10137970A (en) 1996-11-11 1998-05-26 Amada Eng Center:Kk Thermal machining device and its machining head
    JPH10225787A (en) 1997-02-13 1998-08-25 Tanaka Seisakusho Kk Laser beam cutting device and method therefor
    JP3749349B2 (en) 1997-05-08 2006-02-22 株式会社アマダ Laser processing method and laser processing machine
    JPH10318344A (en) 1997-05-20 1998-12-04 Maezawa Kiyuusou Kogyo Kk Pitch advance / retreat mechanism and water faucet with multi-thread screw
    JP3751728B2 (en) 1997-11-07 2006-03-01 小池酸素工業株式会社 Nozzle for piercing
    JPH11314189A (en) 1998-04-28 1999-11-16 Amada Co Ltd Laser beam machining method and its machining head
    JP4162772B2 (en) * 1998-09-09 2008-10-08 日酸Tanaka株式会社 Laser piercing method and laser cutting apparatus
    JP3198095B2 (en) * 1998-10-21 2001-08-13 ファナック株式会社 Laser processing equipment

    Cited By (3)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    EP1145796A1 (en) * 2000-04-10 2001-10-17 Tanaka Engineering Works, Ltd. Piercing device for laser cutter
    US6492617B2 (en) 2000-04-10 2002-12-10 Tanaka Engineering Works, Ltd. Piercing device for laser cutter
    DE102006040784B4 (en) * 2005-09-07 2015-06-25 Disco Corp. Laser beam processing machine

    Also Published As

    Publication number Publication date
    US20020053556A1 (en) 2002-05-09
    US6335507B1 (en) 2002-01-01
    EP1005945A3 (en) 2004-05-12
    US6608279B2 (en) 2003-08-19
    JP3198095B2 (en) 2001-08-13
    JP2000126889A (en) 2000-05-09

    Similar Documents

    Publication Publication Date Title
    US6335507B1 (en) Laser-beam machining method, laser-beam machining device and auxiliary tool for piercing
    JP3056723B1 (en) Laser processing equipment
    JP5276699B2 (en) Laser processing method and laser processing apparatus for piercing
    US9956648B2 (en) Piercing metal workpieces by a laser beam
    JP2007196373A (en) Combined apparatus for cutting material by means of milling cutter and laser radiation
    JP3749349B2 (en) Laser processing method and laser processing machine
    JP2008515643A (en) Hard material processing apparatus and processing method using laser having irradiance in the range of 106 to 109 Wcm-2 and repetition rate in the range of 10 to 50 kHz
    JPH0639571A (en) Laser beam cutting method and device therefor
    CN101678508B (en) Laser processing method for components with edges
    KR20170043252A (en) Burr rejection possible friction stir welding apparatus
    JPH11314189A (en) Laser beam machining method and its machining head
    JPH0947888A (en) Laser piercing method and apparatus thereof
    JPS5964191A (en) Laser working device
    JPH115179A (en) Friction welding method
    JP2005046849A (en) Laser beam machining method and laser beam machining apparatus
    KR100507499B1 (en) A laser head for brazing
    JPS609606A (en) Laser-cut chip cutting tool
    JP4083649B2 (en) Cutting method of bobbin wound steel wire
    JP2718224B2 (en) Laser cutting method
    JPH04200891A (en) Laser piercing method and device therefor
    JPH01228695A (en) Laser beam machining method
    JP4566840B2 (en) Reflector mirror drilling method
    JP2006346716A (en) Laser processing method
    JPH0323275B2 (en)
    JPH11123580A (en) Method and device for preventing fire in laser beam machine

    Legal Events

    Date Code Title Description
    PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

    Free format text: ORIGINAL CODE: 0009012

    AK Designated contracting states

    Kind code of ref document: A2

    Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

    AX Request for extension of the european patent

    Free format text: AL;LT;LV;MK;RO;SI

    PUAL Search report despatched

    Free format text: ORIGINAL CODE: 0009013

    AK Designated contracting states

    Kind code of ref document: A3

    Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

    AX Request for extension of the european patent

    Extension state: AL LT LV MK RO SI

    RIC1 Information provided on ipc code assigned before grant

    Ipc: 7B 23K 26/38 B

    Ipc: 7B 23K 26/14 B

    Ipc: 7B 23K 26/00 A

    17P Request for examination filed

    Effective date: 20040806

    AKX Designation fees paid

    Designated state(s): DE

    STAA Information on the status of an ep patent application or granted ep patent

    Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

    18D Application deemed to be withdrawn

    Effective date: 20060328